Impact modeling of foam cored sandwich plates with ductile or brittle faceplates

被引:54
作者
Rajaneesh, A. [1 ]
Sridhar, I. [1 ]
Rajendran, S. [1 ]
机构
[1] Nanyang Technol Univ, Sch Mech & Aerosp Engn, Singapore 639798, Singapore
关键词
Metal foam; Impact; Metal and composite faceplates; Failure criterion; ALUMINUM FOAMS; CONSTITUTIVE MODELS; DAMAGE INITIATION; METALLIC FOAMS; PANELS; BEHAVIOR; DEFORMATION; INDENTATION; VALIDATION; FAILURE;
D O I
10.1016/j.compstruct.2011.12.021
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This paper reports numerical results of low velocity impact on open-face sandwich plates with an impactor of 2.65 kg mass hitting with 6.7 m/s velocity. The numerical simulation is done using 3D finite element models in LS-DYNA. The sandwich plates used for the present work have a core made of commercial aluminum alloy foam (Alporas) with faceplates made of either ductile aluminum (Al) or brittle carbon fiber reinforced plastic (CFRP). Selection of suitable constitutive models and erosion criterion for the failure analysis is investigated. A simplified analytical model for the peak load prediction under punch-through failure mode is presented. Numerically predicted contact force versus time, energy absorbed versus time along with the failure modes are compared with the experimental measurements and observations. Within experimental scatter, there is a good agreement between the numerical predictions and experimental measurements. Further more, the analytically predicted peak load values are in excellent agreement with the experimental measurements. (C) 2012 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1745 / 1754
页数:10
相关论文
共 25 条
[1]   Compressive deformation in aluminum foam investigated using a 2D object oriented finite element modeling approach [J].
Adziman, M. F. ;
Deshpande, S. ;
Omiya, M. ;
Inoue, H. ;
Kishimoto, K. .
PROGRESSES IN FRACTURE AND STRENGTH OF MATERIALS AND STRUCTURES, 1-4, 2007, 353-358 :651-+
[2]   An energy-based anisotropic yield criterion for cellular solids and validation by biaxial FE simulations [J].
Alkhader, M. ;
Vural, M. .
JOURNAL OF THE MECHANICS AND PHYSICS OF SOLIDS, 2009, 57 (05) :871-890
[3]  
[Anonymous], CP04
[4]  
ASHBY M. F., 2000, Metal Foams: A Design Guide
[5]   Isotropic constitutive models for metallic foams [J].
Deshpande, VS ;
Fleck, NA .
JOURNAL OF THE MECHANICS AND PHYSICS OF SOLIDS, 2000, 48 (6-7) :1253-1283
[6]  
Fatt MSH, 2001, COMPOS STRUCT, V52, P353
[7]   Low-velocity impact failure of aluminium honeycomb sandwich panels [J].
Foo, C. C. ;
Seah, L. K. ;
Chai, G. B. .
COMPOSITE STRUCTURES, 2008, 85 (01) :20-28
[8]  
Gibson L. J., 1997, CELLULAR SOLIDS STRU, V2nd ed
[9]   Failure of aluminum foams under multiaxial loads [J].
Gioux, G ;
McCormack, TM ;
Gibson, LJ .
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2000, 42 (06) :1097-1117
[10]  
Hallquist J., 1998, LS-Dyna Users Manual